• 제목/요약/키워드: TEST-1

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파킨슨병 환자에서 낙상군과 비낙상군에 대한 버그균형검사의 타당도 (Validating the Berg Balance Test for Patients with Parkinson's Disease)

  • 조규행;우영근;황수진
    • PNF and Movement
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    • 제9권3호
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    • pp.31-39
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    • 2011
  • Purpose : The purpose of this study was to evaluate the criterion-related validity of the Berg balance test between fallers and non-fallers in individuals with Parkinson's disease. Methods : Thirty-one patients were recruited for this study. Their initial diagnosis had been made on average $30.1{\pm}10.1$ years earlier. Score of Berg balance test showed significant correlations with indicators of motor functioning and daily living capacity. Berg balance test score was inversely associated with the unified Parkinson's disease rating scale-motor score, and Schwab and England activities of daily living rating scale. Results : In all 3 correlations, lower scores on the Berg balance test correlated with higher unified Parkinson's disease rating scale-motor scores. Results support the criterion-related validity of the Berg balance test. Conclusion : Our research results agree with other published research in suggesting that the Berg balance test may be used as a screening tool and ongoing assessment tool for patients with Parkinson's disease.

스크램제트 엔진 흡입구 시험을 위한 자유제트형 지상추진시험설비의 마하 5 성능 검증 (Mach 5 Performance Verification of Free-jet Type Ground Propulsion Test Facility for Scramjet Engine Intake Test)

  • 이양지;양인영;이경재;오중환;최진
    • 한국추진공학회지
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    • 제26권1호
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    • pp.77-87
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    • 2022
  • 한국항공우주연구원 스크램제트 엔진 시험설비를 활용한 스크램제트 엔진 흡입구 지상 시험을 수행하기 위하여 일반적으로 진행하는 시험 가능 여부 확인 절차를 소개하였다. 스크램제트 흡입구 시험을 수행하기 위하여 새롭게 제작된 마하 5 노즐의 설계 과정을 정리하였으며, 노즐의 코어 유동 분포를 확인하기 위한 장치를 설명하고 코어 유동 시험 분석 결과를 기록하였다. 일련의 시험 결과를 통하여 흡입구가 신규 마하 5 노즐 코어에 위치하는 것을 확인하였다.

통합 개발환경에서 데브옵스 기반 테스트 자동화 모듈 개발에 대한 연구 (A Study of the DEVOPS Test Automation Module for Integrated Development Environment)

  • 정광락;김선주
    • 융합보안논문지
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    • 제22권1호
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    • pp.3-9
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    • 2022
  • 개발 프로젝트의 소프트웨어 개발에 있어서 통합 개발환경의 역할은 매우 중요하다. 다수의 개발자가 각기 다른 모듈을 개발하면 컴파일과 디버깅, 그리고 통합과 테스트, 배포 등의 과정을 거치면서 제품이 완성된다. 하지만, 개발 과정에서의 버그나 각종 이슈 등은 소프트웨어 제품의 품질저하 및 요구사항 불만족 등의 문제를 발생시키게 되었고, 해당 문제를 회피하고 품질 향상을 위해 자동화 테스트의 필요성이 증가되었다. 본 연구에서는 통합 개발환경에서의 테스트 자동화를 통해 개발 프로세스 전 과정에서의 품질향상을 위한 4가지 관점의 테스트 자동화 모듈을 제안한다. 각 자동화 모듈은 데브옵스(DEVOPS) 방법으로 구현된 통합빌드프레임워크의 툴 체인 형태로 연결되어 구동된다.

Z시험에 의한 선회권의 작도법에 관한 연구 (A Study on the Method of Turning Circle Drawing by Z-test)

  • 오정철
    • 한국항해학회지
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    • 제7권1호
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    • pp.33-62
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    • 1983
  • A navigator on bridge needs to know every kinds of motion characteristics of his vessel at sea. Generally when a vessel is completely built, the shipyard makes turning circle diagrams from the results of turing circle tests made during the sea trials for the reference of the vessel's owner. But referring only the data of a turning circle diagram, an officer on bridge can not figure out his vessel's maneuvering characteristics sufficiently, So nowadays the shipyard often adds Z test to turning circle test for more detail references. In this paper the author made Z and turning circle tests at the rudder angles of 15 and and 35 degress separately and in each of the case made a turrning circle diagram from the results of the turning circle test and the esults numerically calculated from mathematical formula made on the base of the maneuvering indices got from the Z test and compared them each other for the purpose of finding the correlations between them. Followings are concluded from the results. An actual turning circle diagram and a calculated one from the results of the Z test at same rudder angle coincides each other well when the center of the calculated circle is transferred by 1.7B toward the direction of the initial turning perpendicularly to the original course and 0.5L toward the direction in parallel with original course in case of the rudder angle of 35 degrees and 1.2B and 0.3L toward each of the above mentioned directions in case of rudder angle of 15 degrees.

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컴팩트형 VAV 공조기의 성능평가와 경제성 분석에 관한 연구 (A Study on Economic Analysis and Performance Appraisal of Compact Type Variable Air Volume)

  • 김동철;정광섭;김영일
    • 설비공학논문집
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    • 제27권1호
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    • pp.44-49
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    • 2015
  • Ceiling cooling and heating system that consider load arrangement and space in the ceiling needs to be developed. Therefore, experimental and economic changes were done to verify the performance of compact type VAV. The test results were as follow. 1) Noise test result, measuring approximately 50.4 dB~56.6 dB (before ceiling in landfill), had a better ceiling deadline than the current measure, about a 10 dB noise reduction, so that the office baseline (40~50 dB) noise was judged to be less than test. 2) For the static pressure test result, taking out an outside hydrostatic 25 mmAq, 24.8 mmAq was measured, respectively, at the point. 3) For the life-cycle cost analysis result, the initial investment cost, maintenance replacement costs, and maintenance costs increased 0.2%, but the energy savings ratio was 19.5% while the whole life cycle savings of 40 years LCC was reduced 11.9%.

장기폭기시킨 축사뇨오수의 벼재배 시비효과 (The Fertilizing Effect of the Long-Time Aerated Animal Wastewater for the Paddy Rice)

  • 오인환
    • 한국축산시설환경학회지
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    • 제3권1호
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    • pp.35-42
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    • 1997
  • The purpose of this study is to investigate the effect of the biologically treated animal wastewater as a liquid fertilizer in the paddy rice. The treated water has content of the ammonia nitrogen 24mg/I and nitrate 40 mg/I on an average in the first year. A trace of nitrite has been shown. The phosphate content was 92 mg/I on an average. The amount of yielded rice was 365kg/10a for test 1 (no fertilizer), 388dg/10a for test 2(chemical fertilizer), 526kg/10a for test 3 (treated water) respectively. The treated water showed 35% more in production than the chemical fertilizer. The treated water has content of the ammonia nitrogen 40mg/I and nitrate 67mg/I on an average in the second year. A trace of nitrite has been shown. The phosphate content was 57mg/I on an average. The amount of yielded rice was 402kg/10a for test 1, 505kg/10a for test 2, 607kg/10a for test 3 respectively. Yield of unhulled rice was 20% more in the plot of treated water than that of chemical fertilizer.

TSV 기반 3D IC Pre/Post Bond 테스트를 위한 IEEE 1500 래퍼 설계기술 (IEEE 1500 Wrapper Design Technique for Pre/Post Bond Testing of TSV based 3D IC)

  • 오정섭;정지훈;박성주
    • 전자공학회논문지
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    • 제50권1호
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    • pp.131-136
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    • 2013
  • 칩 적층기술의 발달로 TSV(Through Silicon Via) 기반 3D IC가 개발되었다. 3D IC의 높은 신뢰성과 수율을 얻기 위해서는 pre-bond 와 post-bond 수준에서 다양한 TSV 테스트가 필수적이다. 본 논문에서는 pre-bond 다이의 TSV 연결부에서 발생하는 미세한 고장과 post-bond 적층된 3D IC의 TSV 연결선에서 발생하는 다양한 고장을 테스트할 수 있는 설계기술을 소개한다. IEEE 1500 표준 기반의 래퍼셀을 보완하여 TSV 기반 3D IC pre-bond 및 post-bond의 at speed test를 통하여 known-good-die와 무결점의 3D IC를 제작하고자 한다.

1차원 압밀점토의 응력해방에 의한 수직변형량과 현장재현 압밀시험에 관한 연구 (A study on reappeared consolidation test of in-situ property and vertical deformation of sample due to stress release)

  • 김재영;;강상욱;김기섭;박상욱;김성래
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2008년도 춘계 학술발표회 초청강연 및 논문집
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    • pp.1-6
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    • 2008
  • When a saturated clay is sampled in an undisturbed manner from a bore hole, the sample extends vertically and shrinks horizontally under undrained conditions due to stress release. The conventional consolidation test specimen is trimmed from the expanded sample so that its diameter is equal to the inner diameter of the consolidation test ring, this test procedure does not reproduce the actual consolidation behavior. The measurement of sample extension was conducted by means of overcoring method found that the extension strains were 1 to 2%. To simulate the in-situ consolidation behavior, the consolidation test method that uses a specimen with a slightly smaller diameter than the inside diameter of consolidometer so that the specimen expands laterally to the inside of the ring.

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EM시험에서의 Joule Heating 영향 및 초기저항값 (Joule Heating Effects and Initial Resistance in Electromigration Test)

  • 주철원;강형곤;한병성
    • 대한전기학회논문지:전기물성ㆍ응용부문C
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    • 제48권6호
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    • pp.436-441
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    • 1999
  • Joule heating effect in EM(Electromigration) test were performed on a bend test structure. EM test is done under high current densities(1.0-2.5MA/cm2), which leads to joule heating. Since joule heating is added to the controlled oven(stress) temperature, themetal line temperature is higher than the stress temperature. The increase in the stress temperature due to joule heating is important because EM phenomena and metal line failure are related to the stress temperature. In this paper, metal line was stressed with a current density of 1.0 MA/$cm^2$, 1.5MA/$cm^2$, 2.0MA/$cm^2$, 2.5MA/$cm^2$, for 1200 sec and temperature increase due to joule heating was less than $10^{\circ}C$. Also it took 30 minutes for the metal line to equalized with oven temperature. Recommendations are given for the EM test to determine the initial resistance of EM test structure under stress temperature and current density.

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가스터빈엔진 고공성능시험설비의 측정불확도 개선 (Improving the Measurement Uncertainty of Altitude Test Facility for Gas Turbine Engines)

  • 이대성;양인영;전용민;김춘택;양수석
    • 대한기계학회논문집B
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    • 제26권11호
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    • pp.1496-1502
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    • 2002
  • An Altitude Engine Test Facility(AETF) was built at the Korea Aerospace Research Institute in October 1999 and has been being operated for altitude testing of gas turbine engines of 3,000 Ibf class or less. The AETF has been calibrated using several engines such as J69 of Teledyne Co. as a facility checkout engine. Uncertainty analyses on the air flow rate and thrust were performed using the test results, according to ASME PTC 19.1-1998. Several modifications on the facility and test method were made in order to improve the measurement uncertainty to a satisfactory level over the whole operating envelop. Spatial distributions of pressure and temperature were measured, sensors were substituted by more accurate ones, inlet duct was modified to refine the flow quality, and pressure control logic was revised to remove the cell pressure fluctuation. As a result, the uncertainty of the air flow measurement was improved by 0.1% over all the test conditions, and the net thrust measurement by up to 3%. The improved measurement uncertainties of air flow and thrust are 0.68~O.73% and 0.4~1.3%, respectively.